A semiempirical theory is presented based on Cheng's analysis of slender blunted cones at zero angle of attack, while the tangent cone approximation is used to account for angle-of-attack effects. Quasi steady-state conditions are assumed to be valid.
Hypersonic Stability Derivatives of Blunted Slender Cones
1964
2 pages
Report
Keine Angabe
Englisch
Pressure correlation for blunted slender cones.
AIAA | 1969
|Hypersonic Flow Over Blunted Slender Wedges
AIAA | 1974
|Far-wake behavior of hypersonic blunted cones.
AIAA | 1967
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